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dc.contributor.authorПосадов, В.В.
dc.date2016
dc.date.accessioned2025-08-22T12:22:04Z-
dc.date.available2025-08-22T12:22:04Z-
dc.date.issued2016
dc.identifier.identifierDspace\SGAU\20161121\60003
dc.identifier.citationМатериалы докладов междунар. науч.-техн. конф. 22-24 июня 2016 г. Ч. 1, с. 195-196
dc.identifier.isbn978-5-7883-1084-8
dc.identifier.urihttp://repo.ssau.ru/jspui/handle/123456789/14462-
dc.descriptionУДК 534.629.7.036.3
dc.description.abstractThis research contains analysis of external factors that affects the beginning of aerodynamic and aeroelastic oscillations in compressor of gas turbine engine. Has been developed the flutter and rotating stall diagnostics method. This method is based on frequency response characteristics. Type of oscillations is determined when signal magnitude reaches corresponding threshold (predicted taken into account operating conditions of the engine).
dc.languagerus
dc.publisherСамарский университет
dc.titleМетод вибрационной диагностики аэродинамических и аэроупругих колебаний в компрессоре газотурбинного двигателя термоэлектронной эмиссии
dc.title.alternativeDiagnostics method of aerodynamic and aeroelastic oscillations in the gas turbine engine compressor
dc.typeArticle
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Metod-vibracionnoi-diagnostiki-aerodinamicheskih-i-aerouprugih-kolebanii-v-kompressore-gazoturbinnogo-dvigatelya-60003
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Metod-vibracionnoi-diagnostiki-aerodinamicheskih-i-aerouprugih-kolebanii-v-kompressore-gazoturbinnogo-dvigatelya-60003
Appears in Collections:Проблемы и перспективы развития двигателестроения

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